[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 17th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 562 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
292/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 220
1
297/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 220
7
301/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2019/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4780322
62 A = 6791519
21 meter
Y = -1041962
94 meter E =
0013049
Z = -4720101
08 I = 51
96423
XDOT = -1282
764517 Wp = 102
12473
YDOT = 6985
914030 meter/sec RA = 118
70306 deg
ZDOT = -2850
584778 TA = 139
70161
MA = 139
60483
Ha = 229
084 n
mi
Hp = 219
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15683473
16 X = 4814547
11
Y = -3418513
57 feet Y = -988314
85 meter
Z = -15485895
92 Z = -4696796
27
XDOT = -4208
545002 XDOT = -1346
940766
YDOT = 22919
665453 feet/sec YDOT = 6971
210288 meter/sec
ZDOT = -9352
312265 ZDOT = -2856
972334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13060857
66 X = -3980949
42
Y = 9505460
28 feet Y = 2897264
29 meter
Z = -15379556
56 Z = -4687688
84
XDOT = -4772
991232 XDOT = -1454
807728
YDOT = -21688
055578 feet/sec YDOT = -6610
519340 meter/sec
ZDOT = -9381
852831 ZDOT = -2859
588743
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19289
52125135
00016717 00000-0 10270-3 0 9000
2 25544 51
6379 119
6194 0006812 156
1555 203
9912 15
50199261 34078
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
52125135 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 119
6194 deg
Eccentricity:
0006812
Arg of perigee: 156
1555 deg
Mean anomaly: 203
9912 deg
Mean motion: 15
50199261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 312
Coasting Arc #2 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2019/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4609615
75 A = 6790920
52 meter
Y = 992376
04 meter E =
0013010
Z = 4883568
65 I = 51
97667
XDOT = 1066
909694 Wp = 139
56750
YDOT = -7182
116457 meter/sec RA = 113
76848 deg
ZDOT = 2453
223857 TA = 286
38653
MA = 286
52952
Ha = 229
108 n
mi
Hp = 219
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15123411
26 X = -4644092
48
Y = 3255826
89 feet Y = 940635
41 meter
Z = 16022206
86 Z = 4861092
51
XDOT = 3500
359889 XDOT = 1135
226194
YDOT = -23563
374204 feet/sec YDOT = -7169
803477 meter/sec
ZDOT = 8048
634701 ZDOT = 2458
572755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12458604
33 X = 3797382
60
Y = -9347587
14 feet Y = -2849144
56 meter
Z = 15919638
25 Z = 4852305
74
XDOT = 6078
113964 XDOT = 1852
609136
YDOT = 21925
480154 feet/sec YDOT = 6682
886351 meter/sec
ZDOT = 8073
472395 ZDOT = 2460
794386
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19290
55269493
00016717 00000-0 10270-3 0 9012
2 25544 51
6376 114
5077 0006762 159
8044 200
3376 15
50168488 34236
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
55269493 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 114
5077 deg
Eccentricity:
0006762
Arg of perigee: 159
8044 deg
Mean anomaly: 200
3376 deg
Mean motion: 15
50168488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 322
Coasting Arc #3 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2019/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4467342
26 A = 6790161
20 meter
Y = -867925
30 meter E =
0014735
Z = -5050743
53 I = 51
98665
XDOT = -840
282843 Wp = 103
39714
YDOT = 7335
095890 meter/sec RA = 108
83380 deg
ZDOT = -2011
936288 TA = 147
15457
MA = 147
06291
Ha = 228
979 n
mi
Hp = 219
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14656634
71 X = 4501249
93
Y = -2847523
94 feet Y = -817778
77 meter
Z = -16570680
88 Z = -5028959
97
XDOT = -2756
833475 XDOT = -912
470454
YDOT = 24065
275230 feet/sec YDOT = 7325
295615 meter/sec
ZDOT = -6600
840839 ZDOT = -2016
193550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12056725
59 X = -3674889
96
Y = 8991413
10 feet Y = 2740582
71 meter
Z = -16471267
61 Z = -5020442
37
XDOT = -7374
939310 XDOT = -2247
881502
YDOT = -21967
779409 feet/sec YDOT = -6695
779164 meter/sec
ZDOT = -6620
731402 ZDOT = -2017
998931
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19291
51967184
00016717 00000-0 10270-3 0 9022
2 25544 51
6374 109
7153 0006960 163
0234 197
1151 15
50200240 34386
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
51967184 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 109
7153 deg
Eccentricity:
0006960
Arg of perigee: 163
0234 deg
Mean anomaly: 197
1151 deg
Mean motion: 15
50200240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 292
Coasting Arc #4 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2019/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4343453
51 A = 6789748
40 meter
Y = 769443
53 meter E =
0011010
Z = 5159125
48 I = 51
99535
XDOT = 572
924284 Wp = 149
64759
YDOT = -7476
247456 meter/sec RA = 103
89982 deg
ZDOT = 1586
649806 TA = 285
05940
MA = 285
18121
Ha = 228
980 n
mi
Hp = 219
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14250175
55 X = -4376795
52
Y = 2524421
02 feet Y = 720685
51 meter
Z = 16926264
71 Z = 5137945
20
XDOT = 1879
672847 XDOT = 648
776047
YDOT = -24528
370919 feet/sec YDOT = -7469
416508 meter/sec
ZDOT = 5205
543983 ZDOT = 1589
617106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11685156
96 X = 3561635
84
Y = -8726989
62 feet Y = -2659986
44 meter
Z = 16829598
94 Z = 5129661
76
XDOT = 8769
385863 XDOT = 2672
908811
YDOT = 21875
846815 feet/sec YDOT = 6667
758109 meter/sec
ZDOT = 5219
580713 ZDOT = 1590
928201
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19292
55111439
00016717 00000-0 10270-3 0 9032
2 25544 51
6381 104
6034 0006846 167
1054 193
0273 15
50168292 34542
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
55111439 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 104
6034 deg
Eccentricity:
0006846
Arg of perigee: 167
1054 deg
Mean anomaly: 193
0273 deg
Mean motion: 15
50168292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 298
Coasting Arc #5 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4038656
10 A = 6788894
78 meter
Y = 1120342
80 meter E =
0017709
Z = -5354894
92 I = 51
99882
XDOT = -1770
005542 Wp = 113
81801
YDOT = 7439
196168 meter/sec RA = 102
12418 deg
ZDOT = 215
099487 TA = 158
26454
MA = 158
18929
Ha = 228
828 n
mi
Hp = 220
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13250184
05 X = 4051839
54
Y = 3675665
36 feet Y = 1165579
66 meter
Z = -17568552
90 Z = -5335244
24
XDOT = -5807
104797 XDOT = -1854
106094
YDOT = 24406
811575 feet/sec YDOT = 7418
932480 meter/sec
ZDOT = 705
706978 ZDOT = 206
297090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10700345
44 X = 3261465
29
Y = 8815865
34 feet Y = 2687075
76 meter
Z = -17478989
38 Z = -5327595
96
XDOT = -14633
606466 XDOT = -4460
323251
YDOT = 19121
982930 feet/sec YDOT = 5828
380397 meter/sec
ZDOT = 665
048079 ZDOT = 202
706655
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19292
87343845
00016717 00000-0 10270-3 0 9046
2 25544 51
6415 103
0084 0006854 168
2583 191
8729 15
50180065 34595
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87343845 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 103
0084 deg
Eccentricity:
0006854
Arg of perigee: 168
2583 deg
Mean anomaly: 191
8729 deg
Mean motion: 15
50180065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 325
Coasting Arc #6 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4025609
15 A = 6788894
15 meter
Y = -1262055
41 meter E =
0006590
Z = 5315153
31 I = 52
00482
XDOT = 1472
258770 Wp = 145
27096
YDOT = -7493
287460 meter/sec RA = 97
19151 deg
ZDOT = -669
039028 TA = 311
05897
MA = 311
11590
Ha = 228
808 n
mi
Hp = 220
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13207379
09 X = -4037015
74
Y = -4140601
72 feet Y = -1307136
43 meter
Z = 17438167
02 Z = 5295570
40
XDOT = 4830
245309 XDOT = 1559
191332
YDOT = -24584
276444 feet/sec YDOT = -7476
337548 meter/sec
ZDOT = -2195
009935 ZDOT = -661
676152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10627605
68 X = -3239294
21
Y = -9040915
76 feet Y = -2755671
12 meter
Z = 17348917
95 Z = 5287950
19
XDOT = 13453
257078 XDOT = 4100
552758
YDOT = -19930
166770 feet/sec YDOT = -6074
714832 meter/sec
ZDOT = -2160
894472 ZDOT = -658
640635
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19293
90487726
00016717 00000-0 10270-3 0 9059
2 25544 51
6412 97
8978 0006790 171
1087 189
0185 15
50218646 34755
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90487726 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 97
8978 deg
Eccentricity:
0006790
Arg of perigee: 171
1087 deg
Mean anomaly: 189
0185 deg
Mean motion: 15
50218646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 348
Coasting Arc #7 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4057609
83 A = 6789291
71 meter
Y = 1438837
16 meter E =
0017084
Z = -5263811
26 I = 52
00939
XDOT = -1177
489608 Wp = 121
26219
YDOT = 7473
988818 meter/sec RA = 92
25811 deg
ZDOT = 1129
406949 TA = 159
56888
MA = 159
50046
Ha = 228
619 n
mi
Hp = 220
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13312368
21 X = 4066787
73
Y = 4720594
37 feet Y = 1484263
52 meter
Z = -17269721
97 Z = -5244078
39
XDOT = -3863
154883 XDOT = -1266
464502
YDOT = 24520
960688 feet/sec YDOT = 7460
323811 meter/sec
ZDOT = 3705
403377 ZDOT = 1123
470955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10659121
73 X = 3248900
30
Y = 9433139
55 feet Y = 2875220
93 meter
Z = -17179797
95 Z = -5236402
42
XDOT = -12156
281858 XDOT = -3705
234710
YDOT = 20469
678083 feet/sec YDOT = 6239
157880 meter/sec
ZDOT = 3677
782443 ZDOT = 1120
988089
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19294
87185268
00016717 00000-0 10270-3 0 9063
2 25544 51
6418 93
1059 0006759 175
0888 185
0330 15
50182878 34909
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
87185268 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 93
1059 deg
Eccentricity:
0006759
Arg of perigee: 175
0888 deg
Mean anomaly: 185
0330 deg
Mean motion: 15
50182878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 346
Coasting Arc #8 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110698
27 A = 6789555
69 meter
Y = -1579219
40 meter E =
0005797
Z = 5163236
20 I = 52
00983
XDOT = 884
863724 Wp = 132
89101
YDOT = -7449
756051 meter/sec RA = 87
32563 deg
ZDOT = -1576
809469 TA = 332
22211
MA = 332
25306
Ha = 228
619 n
mi
Hp = 220
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486542
89 X = -4117813
85
Y = -5181166
01 feet Y = -1625227
81 meter
Z = 16939751
32 Z = 5143250
53
XDOT = 2903
096206 XDOT = 975
762633
YDOT = -24441
456861 feet/sec YDOT = -7439
352665 meter/sec
ZDOT = -5173
259412 ZDOT = -1572
290156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10813915
59 X = -3296081
47
Y = -9740001
34 feet Y = -2968752
41 meter
Z = 16848682
40 Z = 5135478
40
XDOT = 10851
783457 XDOT = 3307
623598
YDOT = -20945
067360 feet/sec YDOT = -6384
056531 meter/sec
ZDOT = -5152
089984 ZDOT = -1570
357027
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19295
90329108
00016717 00000-0 10270-3 0 9072
2 25544 51
6407 87
9947 0006741 177
8718 182
2462 15
50222100 35063
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
90329108 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 87
9947 deg
Eccentricity:
0006741
Arg of perigee: 177
8718 deg
Mean anomaly: 182
2462 deg
Mean motion: 15
50222100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 319
Coasting Arc #9 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4210374
84 A = 6790202
58 meter
Y = 1738703
38 meter E =
0015549
Z = -5048906
80 I = 52
01056
XDOT = -608
877205 Wp = 129
42669
YDOT = 7354
073697 meter/sec RA = 82
39259 deg
ZDOT = 2019
342145 TA = 160
17039
MA = 160
10988
Ha = 228
360 n
mi
Hp = 220
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13813565
74 X = 4215144
27
Y = 5704407
41 feet Y = 1785813
22 meter
Z = -16564654
87 Z = -5028442
66
XDOT = -1997
628624 XDOT = -700
876282
YDOT = 24127
538375 feet/sec YDOT = 7346
750488 meter/sec
ZDOT = 6625
138272 ZDOT = 2016
160655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11103990
87 X = 3384496
42
Y = 10155615
03 feet Y = 3095431
46 meter
Z = -16471415
35 Z = -5020487
40
XDOT = -9496
984764 XDOT = -2894
680956
YDOT = 21133
866071 feet/sec YDOT = 6441
602378 meter/sec
ZDOT = 6610
067680 ZDOT = 2014
748629
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19296
87026344
00016717 00000-0 10270-3 0 9086
2 25544 51
6424 83
2026 0006614 182
5930 177
5187 15
50189210 35219
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
87026344 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 83
2026 deg
Eccentricity:
0006614
Arg of perigee: 182
5930 deg
Mean anomaly: 177
5187 deg
Mean motion: 15
50189210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 309
Coasting Arc #10 (Orbit 3536)
---------------------------------------
Vector Time (GMT): 2019/297/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4325150
65 A = 6790705
62 meter
Y = -1857819
27 meter E =
0006251
Z = 4888539
45 I = 52
00545
XDOT = 347
250588 Wp = 118
55966
YDOT = -7255
658160 meter/sec RA = 77
45992 deg
ZDOT = -2450
714499 TA = 355
36900
MA = 355
37478
Ha = 228
356 n
mi
Hp = 220
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14190126
81 X = -4327800
64
Y = -6095207
57 feet Y = -1906200
68 meter
Z = 16038515
25 Z = 4867522
89
XDOT = 1139
273584 XDOT = 440
264020
YDOT = -23804
652755 feet/sec YDOT = -7251
255037 meter/sec
ZDOT = -8040
401899 ZDOT = -2448
801306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11500873
36 X = -3505466
20
Y = -10454821
82 feet Y = -3186629
69 meter
Z = 15942767
59 Z = 4859355
56
XDOT = 8188
466939 XDOT = 2495
844723
YDOT = -21251
863683 feet/sec YDOT = -6477
568051 meter/sec
ZDOT = -8031
113255 ZDOT = -2447
883320
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19297
90169910
00016717 00000-0 10270-3 0 9099
2 25544 51
6407 78
0910 0006556 185
1709 174
9375 15
50228236 35371
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
90169910 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 78
0910 deg
Eccentricity:
0006556
Arg of perigee: 185
1709 deg
Mean anomaly: 174
9375 deg
Mean motion: 15
50228236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3537
Checksum: 334
Coasting Arc #11 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1800659
81 A = 6794768
18 meter
Y = 5360458
90 meter E =
0013268
Z = 3764661
40 I = 52
01685
XDOT = -4456
179752 Wp = 125
68378
YDOT = -4521
215905 meter/sec RA = 77
24769 deg
ZDOT = 4288
179068 TA = 278
99158
MA = 279
14172
Ha = 228
183 n
mi
Hp = 220
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5907676
54 X = -1878755
06
Y = 17586807
42 feet Y = 5339886
23 meter
Z = 12351251
30 Z = 3755724
34
XDOT = -14620
012310 XDOT = -4426
120876
YDOT = -14833
385514 feet/sec YDOT = -4570
879719 meter/sec
ZDOT = 14068
828964 ZDOT = 4266
605624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6109152
22 X = -1862069
60
Y = 17546808
90 feet Y = 5348267
35 meter
Z = 12310061
03 Z = 3752106
60
XDOT = -13334
880114 XDOT = -4064
471459
YDOT = -14485
796237 feet/sec YDOT = -4415
270693 meter/sec
ZDOT = 13970
746114 ZDOT = 4258
283416
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19297
96616384
00016717 00000-0 10270-3 0 9109
2 25544 51
6389 77
7719 0006571 186
9777 173
1284 15
50223730 35389
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96616384 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 77
7719 deg
Eccentricity:
0006571
Arg of perigee: 186
9777 deg
Mean anomaly: 173
1284 deg
Mean motion: 15
50223730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 352
Coasting Arc #12 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1675643
52 A = 6793876
54 meter
Y = -5184677
78 meter E =
0007082
Z = -4059896
35 I = 52
00493
XDOT = 4693
931081 Wp = 126
30134
YDOT = 4594
215320 meter/sec RA = 72
31628 deg
ZDOT = -3938
544763 TA = 103
00185
MA = 102
92277
Ha = 228
167 n
mi
Hp = 220
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5497518
11 X = 1753216
63
Y = -17010097
70 feet Y = -5165506
10 meter
Z = -13319869
93 Z = -4051567
78
XDOT = 15400
036356 XDOT = 4661
339971
YDOT = 15072
884908 feet/sec YDOT = 4646
523666 meter/sec
ZDOT = -12921
734786 ZDOT = -3915
822487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5408866
56 X = 1648622
53
Y = -17068451
72 feet Y = -5202464
08 meter
Z = -13281460
11 Z = -4048189
04
XDOT = 14399
171193 XDOT = 4388
867380
YDOT = 14514
735810 feet/sec YDOT = 4424
091475 meter/sec
ZDOT = -12818
427413 ZDOT = -3907
056676
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19298
93313652
00016717 00000-0 10270-3 0 9110
2 25544 51
6387 72
9792 0006511 189
5070 170
5956 15
50193729 35532
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93313652 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 72
9792 deg
Eccentricity:
0006511
Arg of perigee: 189
5070 deg
Mean anomaly: 170
5956 deg
Mean motion: 15
50193729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 336
Coasting Arc #13 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2019/299/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1549270
39 A = 6792910
72 meter
Y = 5023223
01 meter E =
0012043
Z = 4301556
65 I = 51
99165
XDOT = -4956
491793 Wp = 139
82418
YDOT = -4611
486439 meter/sec RA = 67
38510 deg
ZDOT = 3585
457296 TA = 273
66555
MA = 273
80326
Ha = 227
920 n
mi
Hp = 221
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5082908
10 X = -1626221
44
Y = 16480390
45 feet Y = 5005468
00 meter
Z = 14112718
68 Z = 4293843
47
XDOT = -16261
456015 XDOT = -4921
972996
YDOT = -15129
548685 feet/sec YDOT = -4666
720187 meter/sec
ZDOT = 11763
311340 ZDOT = 3561
464112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4720027
42 X = -1438664
36
Y = 16618186
53 feet Y = 5065223
25 meter
Z = 14077118
67 Z = 4290705
77
XDOT = -15540
974964 XDOT = -4736
889169
YDOT = -14326
759766 feet/sec YDOT = -4366
796377 meter/sec
ZDOT = 11654
221471 ZDOT = 3552
206704
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19299
96457081
00016717 00000-0 10270-3 0 9120
2 25544 51
6396 67
8683 0006558 195
0872 165
0084 15
50233324 35691
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
96457081 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 67
8683 deg
Eccentricity:
0006558
Arg of perigee: 195
0872 deg
Mean anomaly: 165
0084 deg
Mean motion: 15
50233324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 345
Coasting Arc #14 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2019/300/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1491026
57 A = 6792092
36 meter
Y = -4826384
54 meter E =
0007699
Z = -4545203
96 I = 51
97564
XDOT = 5217
114520 Wp = 110
32032
YDOT = 4608
726661 meter/sec RA = 62
45083 deg
ZDOT = -3189
362390 TA = 127
79326
MA = 127
72351
Ha = 227
866 n
mi
Hp = 221
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4891819
45 X = 1566964
47
Y = -15834594
95 feet Y = -4809286
46 meter
Z = -14912086
48 Z = -4537776
23
XDOT = 17116
517454 XDOT = 5180
683227
YDOT = 15120
494295 feet/sec YDOT = 4666
864263 meter/sec
ZDOT = -10463
787368 ZDOT = -3164
107625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4276939
27 X = 1303611
09
Y = -16043493
55 feet Y = -4890056
83 meter
Z = -14877792
96 Z = -4534751
29
XDOT = 16677
783195 XDOT = 5083
388318
YDOT = 14021
796978 feet/sec YDOT = 4273
843719 meter/sec
ZDOT = -10348
958096 ZDOT = -3154
362428
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19300
93154094
00016717 00000-0 10270-3 0 9139
2 25544 51
6405 63
0754 0006367 197
4285 162
6648 15
50203026 35843
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
93154094 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 63
0754 deg
Eccentricity:
0006367
Arg of perigee: 197
4285 deg
Mean anomaly: 162
6648 deg
Mean motion: 15
50203026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 306
Coasting Arc #15 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 107096
47 A = 6795212
65 meter
Y = 5764537
34 meter E =
0012063
Z = 3594640
77 I = 51
97922
XDOT = -5610
959912 Wp = 126
01605
YDOT = -2691
601716 meter/sec RA = 59
76102 deg
ZDOT = 4466
188256 TA = 276
17340
MA = 276
31082
Ha = 227
829 n
mi
Hp = 221
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 351366
38 X = 25166
51
Y = 18912524
09 feet Y = 5765277
00 meter
Z = 11793440
84 Z = 3594961
81
XDOT = -18408
661128 XDOT = -5602
139507
YDOT = -8830
714291 feet/sec YDOT = -2754
297954 meter/sec
ZDOT = 14652
848610 ZDOT = 4438
953052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6525697
06 X = -1989032
46
Y = -17753856
71 feet Y = -5411375
52 meter
Z = 11794410
65 Z = 3594936
37
XDOT = 19093
039240 XDOT = 5819
558360
YDOT = 2671
834266 feet/sec YDOT = 814
375084 meter/sec
ZDOT = 14528
828907 ZDOT = 4428
387051
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19301
51172151
00016717 00000-0 10270-3 0 9149
2 25544 51
6420 60
1968 0006851 199
4216 160
6674 15
50238629 35933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51172151 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 60
1968 deg
Eccentricity:
0006851
Arg of perigee: 199
4216 deg
Mean anomaly: 160
6674 deg
Mean motion: 15
50238629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 306
Coasting Arc #16 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -182885
01 A = 6794324
09 meter
Y = -5559140
62 meter E =
0005787
Z = -3901407
68 I = 51
95806
XDOT = 5857
625057 Wp = 141
46981
YDOT = 2701
019346 meter/sec RA = 54
82846 deg
ZDOT = -4130
978430 TA = 85
34469
MA = 85
27860
Ha = 227
780 n
mi
Hp = 221
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -600016
44 X = -101756
07
Y = -18238650
32 feet Y = -5560732
18 meter
Z = -12799893
97 Z = -3902098
99
XDOT = 19217
929978 XDOT = 5847
052709
YDOT = 8861
612026 feet/sec YDOT = 2766
464296 meter/sec
ZDOT = -13553
078840 ZDOT = -4102
549150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6822631
79 X = 2079538
17
Y = 16923119
38 feet Y = 5158166
79 meter
Z = -12802554
30 Z = -3902218
55
XDOT = -19950
954455 XDOT = -6081
050918
YDOT = -2092
734469 feet/sec YDOT = -637
865466 meter/sec
ZDOT = -13423
623310 ZDOT = -4091
520385
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19302
47869126
00016717 00000-0 10270-3 0 9151
2 25544 51
6419 55
4057 0006825 202
7986 157
2862 15
50207374 36081
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47869126 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 55
4057 deg
Eccentricity:
0006825
Arg of perigee: 202
7986 deg
Mean anomaly: 157
2862 deg
Mean motion: 15
50207374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 326
Coasting Arc #17 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 259941
36 A = 6793350
27 meter
Y = 5364758
64 meter E =
0011065
Z = 4159483
82 I = 51
93615
XDOT = -6108
692824 Wp = 141
05756
YDOT = -2650
292746 meter/sec RA = 49
89352 deg
ZDOT = 3786
167453 TA = 269
99132
MA = 270
11812
Ha = 227
548 n
mi
Hp = 221
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 852825
99 X = 179726
74
Y = 17600914
17 feet Y = 5367216
91 meter
Z = 13646600
45 Z = 4160551
81
XDOT = -20041
643125 XDOT = -6096
994069
YDOT = -8695
186176 feet/sec YDOT = -2718
539113 meter/sec
ZDOT = 12421
809228 ZDOT = 3756
521271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7110938
23 X = -2167413
97
Y = -16119381
35 feet Y = -4913187
44 meter
Z = 13650981
58 Z = 4160819
18
XDOT = 20733
525709 XDOT = 6319
578636
YDOT = 1297
316885 feet/sec YDOT = 395
422186 meter/sec
ZDOT = 12286
806839 ZDOT = 3745
018725
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19303
51012253
00016717 00000-0 10270-3 0 9169
2 25544 51
6431 50
2945 0006847 207
2785 152
8007 15
50242009 36249
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51012253 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 50
2945 deg
Eccentricity:
0006847
Arg of perigee: 207
2785 deg
Mean anomaly: 152
8007 deg
Mean motion: 15
50242009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 282
Coasting Arc #18 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2019/304/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -265623
85 A = 6792509
45 meter
Y = -5156563
57 meter E =
0005701
Z = -4416162
94 I = 51
91134
XDOT = 6357
717246 Wp = 117
25379
YDOT = 2580
588001 meter/sec RA = 44
95685 deg
ZDOT = -3401
555140 TA = 118
41899
MA = 118
36153
Ha = 227
477 n
mi
Hp = 221
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -871469
31 X = -186490
14
Y = -16917859
49 feet Y = -5159091
35 meter
Z = -14488723
56 Z = -4417261
24
XDOT = 20858
652382 XDOT = 6344
911096
YDOT = 8466
496066 feet/sec YDOT = 2651
612992 meter/sec
ZDOT = -11159
957810 ZDOT = -3370
702020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7139808
38 X = 2176213
59
Y = 15357909
74 feet Y = 4681090
89 meter
Z = -14493249
58 Z = -4417542
47
XDOT = -21460
333567 XDOT = -6541
109671
YDOT = -403
967681 feet/sec YDOT = -123
129349 meter/sec
ZDOT = -11019
450468 ZDOT = -3358
728503
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19304
47708983
00016717 00000-0 10270-3 0 9178
2 25544 51
6438 45
5032 0006744 210
5409 149
5350 15
50210622 36392
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
47708983 = yrday
fracday
Element set: 917
Inclination: 51
6438 deg
RA of node: 45
5032 deg
Eccentricity:
0006744
Arg of perigee: 210
5409 deg
Mean anomaly: 149
5350 deg
Mean motion: 15
50210622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 304
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